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Accidents · NTSB ERA14LA057 · Final report

Piper PA-28-161 accident near Elkmont, Alabama, November 30, 2013

On November 30, 2013 at about 7:16 pm local time, a 1977 Piper PA-28-161, registered N8878E, was destroyed in an accident during maneuvering (low-alt flying) near Elkmont, Alabama. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A stuck exhaust valve, which resulted in a total loss of engine power at low altitude. Contributing to the accident were the pilot’s decision to fly at a low altitude, which reduced his forced landing options when the loss of engine power occurred; and poor long-term engine maintenance, which resulted in the buildup of combustion by-products on exhaust valve parts. Contributing to the pilot’s poor aeronautical decision-making was his underlying attention deficit hyperactivity disorder.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
November 30, 2013 · about 7:16 pm local time
Place
Elkmont, Alabama · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Piper PA-28-161, built 1977 · all PA-28-161s on the register
Registration
N8878E · no longer on the register · serial 28-7716253
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The 18-year-old pilot had obtained his private pilot certificate about 16 months before the accident, bought the airplane 25 days before the accident, and had an estimated 5 hours of flight experience in the airplane at the time of the accident. The pilot was moving the airplane to the airport where it would be permanently based. GPS data indicated that the airplane was maneuvering and descending to about 300 ft above ground level near a small community when it began a climbing turn. A witness reported that, about that time, he heard a "pop" sound and that the engine then lost power. The airplane subsequently descended into a telephone pole, hit the ground, and then slid into and bounced off of a vacant house. Large open fields began about 1,200 ft east and northeast of the airplane's final documented in-flight position before the descent. Postaccident examination of all four engine cylinders revealed extensive deposits of combustion by-products on the exhaust valves, guides, and valve seats, indicating that a stuck exhaust valve likely resulted in the loss of engine power. Review of available maintenance logbooks, which began with entries from almost 15 years before the accident, revealed that the engine's total time in service at that time was 4,377 hours and that the time since major overhaul (TSMO) was 1,995 hours. For a 6-year period ending about 3 years before the accident, no maintenance items were recorded, and there were only 5 hours of operation noted between those dates. The latest annual inspection was completed about 6 months before the accident at an engine TSMO of 2,198 hours. No engine compression results were noted; however, the same technician who completed the inspection did record results about 1 year earlier, and all of the recorded compressions were 70 pounds per square inch or higher at that time. The engine TSMO was 2,203 hours at the time of the accident. An engine manufacturer service instruction recommended that the time between overhauls should be 2,000 hours and noted that "engines that do not accumulate the hourly period of [TSMO]…are recommended to be overhauled in the twelfth year." The evidence indicates that the airplane had a history of poor engine maintenance. The pilot had been diagnosed with and was receiving medication for attention deficit hyperactivity disorder (ADHD), which can cause attention deficits, susceptibility to distraction, and impulsivity and impairments in motor inhibition, reaction time, visual-motor coordination, executive functioning, decision-making, and rule-governed behavior. The pilot did not report either the ADHD or the medication he was using to treat it on his only application for a Federal Aviation Administration medical certificate; if he had reported this information, his medical certification would have been deferred at least until he had undergone extensive neuropsychological evaluation and review. The pilot was maneuvering the airplane, which had a poor engine maintenance history, at a very low altitude. When the engine lost power, the resultant forced landing was made to relatively confined terrain. If the pilot had been flying at a higher altitude, he would have had the option of landing in larger fields. His decision to maneuver as low as he did likely resulted from his ADHD in combination with his age and relatively low flight experience (about 180 total flight hours), which would have made him more susceptible to bad decision-making.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Miscellaneous/other during prior to flight
  2. Loss of engine power (total) during maneuvering (low-alt flying) defining event
  3. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Malfunction
  • factor Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Inadequate inspection
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • factor Personnel issues › Psychological › Cognitive limitation › (general) › Pilot
  • factor Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Not serviced/maintained
  • Environmental issues › Physical environment › Object/animal/substance › Pole › Contributed to outcome
  • Environmental issues › Physical environment › Object/animal/substance › Residence/building › Contributed to outcome

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 180 hours in all; 5 in this make and model
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 4,595 hours
  • Last inspection: annual inspection, May 5, 2013; 5 hours since
  • Maximum gross weight: 2,325 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O-320 SERIES (piston); 4,595 hours total

The flight

  • Departed from: DCU Decatur AL
  • Destination: GZS Pulaski TN
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 180° at 7 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 55°F (13°C), dew point 25°F (-4°C)
  • Altimeter: 30.36 inHg
  • Observation at 7:53 pm from KDCU, 17 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.